CN104743115A - Hollow pipe with lifting force - Google Patents
Hollow pipe with lifting force Download PDFInfo
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- CN104743115A CN104743115A CN201510153708.5A CN201510153708A CN104743115A CN 104743115 A CN104743115 A CN 104743115A CN 201510153708 A CN201510153708 A CN 201510153708A CN 104743115 A CN104743115 A CN 104743115A
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- hollow tubular
- lift
- gas channel
- make
- hollow
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- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
Abstract
The invention relates to a hollow pipe with lifting force. The hollow pipe is characterized in that a cavity in a hollow pipe wall (1A) is divided into two parts as air-flow channels by a partitioning plate, and the speeds of fluids of the two air-flow channels are different, so that the pressure difference is generated at the two sides of the partitioning plate and the hollow pipe (1) generates the lifting force; the hollow pipes (1) with the lifting force are arranged and combined along the circumferences of the plurality of large concentric circles, and the partitioning plates in all the hollow pipes (1) are radially vertical to the large circles, and have the same pressure difference and rotating direction so as to form many cylinders with axial fluid channels capable of generating the lifting force; the gaps among the hollow pipes (1) in the cylinders are provided with the partitioning plates (2) capable of generating the pressure difference at the two sides; the outer sides of the cylinders are wrapped with diaphragms or plates (3), the outer walls of the cylinders are provided with teeth rings or belt rings (4), and the power of a power impeller is transferred to a shaft (5) by a synchronous belt or belt (6) so as to drive a power generator to generate power.
Description
Technical field
Aerodynamic force component and application thereof.
Background technology
At present, the aerodynamic force component with lift mainly contains fixed wing and the rotor blade of aircraft.Its weak point is, complex structure, manufacturing cost are high, lift is limited.
Summary of the invention
The invention provides a kind of hollow tubular and the application thereof with lift for this reason, it is characterized in that: be that two parts are as gas channel using the cavity baffle for separating in hollow tube wall (1A), and make by the fluid velocity of this two parts gas channel different, thus produce pressure reduction in dividing plate both sides, make hollow tubular (1) produce lift.
Make by one of fluid velocity diverse ways of above-mentioned two parts gas channel be: with dividing plate (1B), the cavity in hollow tube wall (1A) is divided into the different two parts of sectional area as gas channel, and make by the fluid velocity of this two parts gas channel different, thus produce pressure reduction in dividing plate both sides, make hollow tubular (1) produce lift.
Make two of the fluid velocity diverse ways by above-mentioned two parts gas channel be: the series connection of the fixed wing (1C) of many aircrafts is placed in the cavity in hollow tubular tube wall (1A), cavity in hollow tubular tube wall (1A) is divided into the different two parts of flow velocity as gas channel by fixed wing (1C), and make by the fluid velocity of this two parts gas channel different, thus produce pressure reduction in dividing plate both sides, make hollow tubular (1) produce lift.
Make three of the fluid velocity diverse ways by above-mentioned two parts gas channel be: with dividing plate (1D), the cavity in hollow tubular tube wall (1A) is divided into the different two parts of fluid resistance as gas channel, wherein the tube wall of a part is smooth, and the tube wall of another part is coarse, make by the fluid velocity of this two parts gas channel different, thus produce pressure reduction in dividing plate both sides, make hollow tubular (1) produce lift.
Above-mentioned three kinds of method synthesis can be used.
The available above-mentioned power turbine with hollow tubular (1) the combination to manufacture fluid electrical generator of lift.Its specific practice is: by the above-mentioned hollow tubular (1) with lift along several large concentric circle permutation and combination, dividing plate in each hollow tubular (1) is vertical with the radial direction of great circle, and pressure reduction rotation direction is identical, form many cylinders with the axial fluid passage that can produce lift; In space between many hollow tubulars (1) in cylinder, be provided with the dividing plate (2) that can produce both sides pressure reduction; Be enclosed with diaphragm or sheet material (3) in cylindrical outside, above-mentioned cylindrical body outer wall is provided with ring gear or strap lug (4), by Timing Belt or belt (6), the power of power turbine is passed to axle (5), drive electrical generators generates electricity.
Compared with traditional various fluid power-generation impellers, the fluid generator power turbine of said structure, due to lightweight, intensity is high, torsion is large, the diameter that can manufacture and power are very large, and can, lower than the impact of high wind, be a kind of desirable fluid power-generation power turbine.
Available above-mentioned hollow tubular (1) combination with lift manufactures the cored slab with lift, as a kind of aircraft.Its specific practice is: combined along rectangular array by the above-mentioned hollow tubular (1) with lift, form the cored slab with lift.Turbine or fanjet are arranged in each hollow tubular (1), its suck and ejection the many fixed wing (1C) of high velocity air in each hollow tubular (1) on produce pressure reduction, bring lift, this aircraft can be made to realize original place take off vertically, be placed on the many fixed wings (1C) in hollow tubular tube wall (1A), can rotate at the same time or separately along the axis of hollow tubular (1), the traversing or pivot turn of aircraft can be made.Because this aircraft has large area, heavy－duty, can consider it can be used as and use atomic driven flying platform, be i.e. a kind of missile carrier.Make the handsets such as fighter plane in landing above and stop.Together fly because missile carrier carries handset, when handset is taken off, what only need depart from machine tool is fixing, just can skid off machine tool voluntarily from rear door and take off; During landing, close with the speed of machine tool until identical owing to controlling, just can drop on machine tool like a cork.
Available above-mentioned hollow tubular (1) combination with lift manufactures the aircraft with larger cavity.Its specific practice is: combined along larger circumferential arrangement by the above-mentioned hollow tubular (1) with lift, form the larger hollow tubular with lift; The cavity of large hollow tubular is cabin, with many hollow tubulars (1) for wing, turbine or fanjet are arranged in each hollow tubular (1), its suck and ejection the many fixed wing (1C) of high velocity air in each hollow tubular (1) on produce pressure reduction, bring lift, this aircraft can be made to realize original place take off vertically, be placed on the many fixed wings (1C) in hollow tubular tube wall (1A), can rotate at the same time or separately along the axis of hollow tubular (1), the traversing or pivot turn of aircraft can be made.
Accompanying drawing explanation
Fig. 1 is the cross-section structure schematic diagram of one of the embodiment of the present invention.
Fig. 2 is the cross-section structure schematic diagram of the embodiment of the present invention two.
Fig. 3 is the cross-section structure schematic diagram of the embodiment of the present invention three.
Fig. 4 is the cross-section structure schematic diagram of the embodiment of the present invention four.
Fig. 5 is the cross-section structure schematic diagram of the embodiment of the present invention five.
Fig. 6 is the cross-section structure schematic diagram of the embodiment of the present invention six.
1. hollow tubulars in figure, the hollow tube wall of 1A., 1B. dividing plate, 1C. fixed wing, 1D. dividing plate, 2. dividing plate, 3. diaphragm or sheet material, 4. ring gear or strap lug, 5. axle, 6. Timing Belt or belt.
Detailed description of the invention
In Fig. 1, with dividing plate (1B), the cavity in hollow tube wall (1A) is divided into the different two parts of sectional area as gas channel, and make by the fluid velocity of this two parts gas channel different, thus produce pressure reduction in dividing plate both sides, make hollow tubular (1) produce lift.
In Fig. 2, the series connection of the fixed wing (1C) of many aircrafts is placed in the cavity in hollow tubular tube wall (1A), cavity in hollow tubular tube wall (1A) is divided into the different two parts of flow velocity as gas channel by fixed wing (1C), and make by the fluid velocity of this two parts gas channel different, thus produce pressure reduction in dividing plate both sides, make hollow tubular (1) produce lift.
In Fig. 3, with dividing plate (1D), the cavity in hollow tubular tube wall (1A) is divided into the different two parts of fluid resistance as gas channel, wherein the tube wall of a part is smooth, and the tube wall of another part is coarse, make by the fluid velocity of this two parts gas channel different, thus produce pressure reduction in dividing plate both sides, make hollow tubular (1) produce lift.
In Fig. 4, the available above-mentioned power turbine with hollow tubular (1) the combination to manufacture fluid electrical generator of lift.Its specific practice is: by the above-mentioned hollow tubular (1) with lift along several large concentric circle permutation and combination, dividing plate in each hollow tubular (1) is vertical with the radial direction of great circle, and pressure reduction rotation direction is identical, form many cylinders with the axial fluid passage that can produce lift; In space between many hollow tubulars (1) in cylinder, be provided with the dividing plate (2) that can produce both sides pressure reduction; Be enclosed with diaphragm or sheet material (3) in cylindrical outside, above-mentioned cylindrical body outer wall is provided with ring gear or strap lug (4), by Timing Belt or belt (6), the power of power turbine is passed to axle (5), drive electrical generators generates electricity.
In Fig. 5, available above-mentioned hollow tubular (1) combination with lift manufactures the cored slab with lift, as a kind of aircraft.Its specific practice is: combined along rectangular array by the above-mentioned hollow tubular (1) with lift, form the cored slab with lift.Turbine or fanjet are arranged in each hollow tubular (1), its suck and ejection the many fixed wing (1C) of high velocity air in each hollow tubular (1) on produce pressure reduction, bring lift, this aircraft can be made to realize original place take off vertically, be placed on the many fixed wings (1C) in hollow tubular tube wall (1A), can rotate at the same time or separately along the axis of hollow tubular (1), the traversing or pivot turn of aircraft can be made.Because this aircraft has large area, heavy－duty, can consider it can be used as and use atomic driven flying platform, be i.e. a kind of missile carrier.Make the handsets such as fighter plane in landing above and stop.Together fly because missile carrier carries handset, when handset is taken off, what only need depart from machine tool is fixing, just can skid off machine tool voluntarily from rear door and take off; During landing, close with the speed of machine tool until identical owing to controlling, just can drop on machine tool like a cork.
In Fig. 6, available above-mentioned hollow tubular (1) combination with lift manufactures the aircraft with larger cavity.Its specific practice is: combined along larger circumferential arrangement by the above-mentioned hollow tubular (1) with lift, form the larger hollow tubular with lift; The cavity of large hollow tubular is cabin, with many hollow tubulars (1) for wing, turbine or fanjet are arranged in each hollow tubular (1), its suck and ejection the many fixed wing (1C) of high velocity air in each hollow tubular (1) on produce pressure reduction, bring lift, this aircraft can be made to realize original place take off vertically, be placed on the many fixed wings (1C) in hollow tubular tube wall (1A), can rotate at the same time or separately along the axis of hollow tubular (1), the traversing or pivot turn of aircraft can be made.
Claims (10)
1. one kind has the hollow tubular of lift, it is characterized in that: be that two parts are as gas channel using the cavity baffle for separating in hollow tube wall (1A), and make by the fluid velocity of this two parts gas channel different, thus produce pressure reduction in dividing plate both sides, make hollow tubular (1) produce lift.
2. a kind of hollow tubular with lift according to claim 1, it is characterized in that: make by one of fluid velocity diverse ways of above-mentioned two parts gas channel be: with dividing plate (1B), the cavity in hollow tube wall (1A) is divided into the different two parts of sectional area as gas channel, and make by the fluid velocity of this two parts gas channel different, thus produce pressure reduction in dividing plate both sides, make hollow tubular (1) produce lift.
3. a kind of hollow tubular with lift according to claim 1, it is characterized in that: make two of the fluid velocity diverse ways by above-mentioned two parts gas channel be: the series connection of the fixed wing (1C) of many aircrafts is placed in the cavity in hollow tubular tube wall (1A), cavity in hollow tubular tube wall (1A) is divided into the different two parts of flow velocity as gas channel by fixed wing (1C), and make by the fluid velocity of this two parts gas channel different, thus produce pressure reduction in dividing plate both sides, make hollow tubular (1) produce lift.
4. a kind of hollow tubular with lift according to claim 1, it is characterized in that: make three of the fluid velocity diverse ways by above-mentioned two parts gas channel be: with dividing plate (1D), the cavity in hollow tubular tube wall (1A) is divided into the different two parts of fluid resistance as gas channel, wherein the tube wall of a part is smooth, and the tube wall of another part is coarse, make by the fluid velocity of this two parts gas channel different, thus produce pressure reduction in dividing plate both sides, make hollow tubular (1) produce lift.
5. a kind of application with the hollow tubular of lift according to claim 1, is characterized in that: by the above-mentioned power turbine with hollow tubular (1) the combination to manufacture fluid electrical generator of lift.
6. a kind of application with the hollow tubular of lift according to claim 5, it is characterized in that: by the above-mentioned hollow tubular (1) with lift along several large concentric circle permutation and combination, dividing plate in each hollow tubular (1) is vertical with the radial direction of great circle, and pressure reduction rotation direction is identical, form many cylinders with the axial fluid passage that can produce lift; In space between many hollow tubulars (1) in cylinder, be provided with the dividing plate (2) that can produce both sides pressure reduction; Be enclosed with diaphragm or sheet material (3) in cylindrical outside, above-mentioned cylindrical body outer wall is provided with ring gear or strap lug (4), by Timing Belt or belt (6), the power of power turbine is passed to axle (5), drive electrical generators generates electricity.
7. a kind of application with the hollow tubular of lift according to claim 1, is characterized in that: manufacture the cored slab with lift, as a kind of aircraft with above-mentioned hollow tubular (1) combination with lift.
8. a kind of application with the hollow tubular of lift according to claim 7, is characterized in that: combined along rectangular array by the above-mentioned hollow tubular (1) with lift, form the cored slab with lift; Turbine or fanjet are arranged in each hollow tubular (1), its suck and ejection the many fixed wing (1C) of high velocity air in each hollow tubular (1) on produce pressure reduction, bring lift, this aircraft can be made to realize original place take off vertically, be placed on the many fixed wings (1C) in hollow tubular tube wall (1A), can rotate at the same time or separately along the axis of hollow tubular (1), the traversing or pivot turn of aircraft can be made.
9. a kind of application with the hollow tubular of lift according to claim 1, is characterized in that: manufacture the aircraft with larger cavity with above-mentioned hollow tubular (1) combination with lift.
10. a kind of application with the hollow tubular of lift according to claim 9, is characterized in that: combined along larger circumferential arrangement by the above-mentioned hollow tubular (1) with lift, form the larger hollow tubular with lift; The cavity of large hollow tubular is cabin, with many hollow tubulars (1) for wing, turbine or fanjet are arranged in each hollow tubular (1), its suck and ejection the many fixed wing (1C) of high velocity air in each hollow tubular (1) on produce pressure reduction, bring lift, this aircraft can be made to realize original place take off vertically, be placed on the many fixed wings (1C) in hollow tubular tube wall (1A), can rotate at the same time or separately along the axis of hollow tubular (1), the traversing or pivot turn of aircraft can be made.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510153708.5A CN104743115A (en) | 2015-04-02 | 2015-04-02 | Hollow pipe with lifting force |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510153708.5A CN104743115A (en) | 2015-04-02 | 2015-04-02 | Hollow pipe with lifting force |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN104743115A true CN104743115A (en) | 2015-07-01 |
Family
ID=53583531
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510153708.5A Pending CN104743115A (en) | 2015-04-02 | 2015-04-02 | Hollow pipe with lifting force |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104743115A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106184747A (en) * | 2015-05-03 | 2016-12-07 | 徐林波 | Wind-tunnel pipe and the application thereof of lateral thrust can be produced |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1216279A (en) * | 1997-12-08 | 1999-05-12 | 佟士俊 | Airflow-sucking airship |
| CN1231977A (en) * | 1998-04-10 | 1999-10-20 | 佟士俊 | Tube wing type helicopter |
| CN1792715A (en) * | 2005-07-17 | 2006-06-28 | 李志文 | Wingless aircraft and implementing thereof |
| CN101143622A (en) * | 2006-09-11 | 2008-03-19 | 李志文 | Wingless air vehicle capable of vertical take-off and landing and its realizing method |
| CN101716995A (en) * | 2009-10-12 | 2010-06-02 | 章成谊 | Waved wing and waved surface of object |
| CN102120490A (en) * | 2010-01-11 | 2011-07-13 | 刘跃东 | Wind tunnel type aircraft |
-
2015
- 2015-04-02 CN CN201510153708.5A patent/CN104743115A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1216279A (en) * | 1997-12-08 | 1999-05-12 | 佟士俊 | Airflow-sucking airship |
| CN1231977A (en) * | 1998-04-10 | 1999-10-20 | 佟士俊 | Tube wing type helicopter |
| CN1792715A (en) * | 2005-07-17 | 2006-06-28 | 李志文 | Wingless aircraft and implementing thereof |
| CN101143622A (en) * | 2006-09-11 | 2008-03-19 | 李志文 | Wingless air vehicle capable of vertical take-off and landing and its realizing method |
| CN101716995A (en) * | 2009-10-12 | 2010-06-02 | 章成谊 | Waved wing and waved surface of object |
| CN102120490A (en) * | 2010-01-11 | 2011-07-13 | 刘跃东 | Wind tunnel type aircraft |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106184747A (en) * | 2015-05-03 | 2016-12-07 | 徐林波 | Wind-tunnel pipe and the application thereof of lateral thrust can be produced |
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| PB01 | Publication | ||
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Application publication date: 20150701 |